A jet engine igniter lead elbow assembly, comprising:
- a saddle adapter, said saddle adapter having a horizontal axis, a cylindrical cross-section of a first predetermined diameter about said horizontal axis, a first end and a second end;
- a first orifice extending from said first end to said second end;
- a semi-circular cut-out disposed at said first end perpendicular to said horizontal axis, said cut-out having a first predetermined radius;
- a master cylinder, said master cylinder having a vertical axis, a cylindrical cross-section of the first predetermined diameter about said vertical axis, an outer surface, a closed lower end, an upper end and a second orifice extending from said closed lower end to said upper end;
- a circular opening, said circular opening being perpendicular to said vertical axis, disposed adjacent said closed lower end and penetrating said outer surface and extending to said second orifice;
- a first necked down section, said first necked down section disposed at said upper end, having a second predetermined diameter less that said first predetermined diameter and extending from said upper end toward said lower end for a first predetermined distance;
- said saddle adapter being removably attached to said master cylinder such that said semi-circular cut-out is disposed over said circular opening in said master cylinder with said first orifice adjoining said second orifice;
- an extension tube, said extension tube having a vertical axis, a cylindrical cross-section of the first predetermined diameter about said vertical axis, a top end, a bottom end and a third orifice extending from said bottom end to said top end;
- said bottom end having a first counter bore, said first counter bore being sized and shaped to fit slidably over said first necked down section of said master cylinder;
- said top end having a second necked down section, said second necked down section having the second predetermined diameter and extending from said top end toward said bottom end for the first predetermined distance;
- a ferrule, said ferrule having a vertical axis, a cylindrical cross-section, a first end, a second end and a first portion adjacent said first end of the first predetermined diameter about said vertical axis;
- a second counter bore, said second counter bore be disposed at said first end of said ferrule and being sized and shaped to fit slidably over said second necked down section of said extension tube;
- a restraining lip, said restraining lip being disposed at said second end of said ferrule and having a third predetermined diameter greater than said first predetermined diameter;
- said ferrule being removably attached at its first end to said top end of said extension tube with said second counter bore fitted slidably over said second necked down section;
- a nut extension tube, said nut extension tube having a vertical axis, an outer surface, a first end, a second end and a hollow cylindrical body disposed about said vertical axis, said hollow body having an internal diameter greater than said first predetermined diameter and smaller than said third predetermined diameter;
- a gripping surface disposed at said first end of said nut extension tube and a threaded receiving section at said second end;
- said threaded receiving section being sized and shaped to fit slidably over said ferrule and said thread being sized and shaped to accommodate a fitting on a jet engine;
- said nut extension tube being fitted over said extension tube and said ferrule;
- said top end of said extension tube being removably attached to said ferrule with said second counter bore fitted slidably over said second necked down section;
- and
- whereby when said extension tube is removably attached to said master cylinder, said nut extension tube will be slidably and rotably held in place by said ferrule.